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GENMAT-1

NORAD 58276 Payload LEO 2023-174W ● Active
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🛰️ Orbital Parameters
Perigee
450 km
Apogee
460 km
Inclination
97.4°
Period
93.7 min
Mean Motion
15.36905988 rev/day
TLE Epoch
2026-11-01 11:00:00 UTC
📐 Computed Orbital Characteristics
Avg. Altitude455 km
Orbital Velocity27,510 km/h
Velocity7.64 km/s
Orbital Period94 minutes
Orbits / Day15.37
Eccentricity0.0007
Semi-Major Axis6,826 km
Orbit ClassSun-Synchronous (SSO)
Est. Orbital Lifetime~1–3 years
🚀 Launch & Identity
Country / Operator
🇺🇸 GenMat (United States)
Launch Date
2023-11-11
Launch Site
Vandenberg Space Force Base, United States
Int'l Designator
2023-174W
Object Type
Payload
RCS Size
Medium (0.1–1 m²)
📖 About This Object
GENMAT-1 is an active satellite operated by GenMat (United States), launched on 2023-11-11 from Vandenberg Space Force Base, United States on the Transporter-9 launch. It orbits in Low Earth Orbit (LEO) at altitudes between 450 km and 460 km with an inclination of 97.4°. It travels at approximately 27,510 km/h (7.64 km/s), completing one full orbit every 94 minutes — that’s roughly 15.37 orbits per day. Its near-polar, sun-synchronous orbit means it passes over any given point on Earth at approximately the same local solar time, ideal for consistent Earth observation lighting conditions. Its near-circular orbit (eccentricity close to zero) means it maintains a very consistent altitude throughout each revolution. At its current altitude, the estimated orbital lifetime before atmospheric re-entry is ~1–3 years. Orbital Radar tracks GENMAT-1 in real time using the latest two-line element set (TLE) data, providing live position, altitude, speed and orbital path updated continuously.
🌍 Orbit Context
GENMAT-1 orbits at an average altitude of 455 km in a sun-synchronous orbit (SSO), a specialised subset of LEO where the orbital plane precesses to maintain a constant angle relative to the Sun. This provides consistent lighting conditions on every pass — essential for Earth observation, weather monitoring and environmental science. Within ±50 km of GENMAT-1’s average altitude, there are currently 10,645 active payloads and 160 tracked debris or rocket body fragments — notable neighbours include ISS (ZARYA), STARLINK-1017, STARLINK-1039. This makes it one of the more crowded altitude bands, containing roughly 56.2% of all active satellites. With an inclination of 97.4°, GENMAT-1 passes over latitudes between 97.4°N and 97.4°S, providing near-global coverage including the polar regions. Polar and near-polar orbits are used for reconnaissance, weather monitoring and Earth-observation missions that need to image every part of the planet. United States operates approximately 13,340 active satellites in total, of which 10,191 share a similar altitude band with GENMAT-1.
❓ Frequently Asked Questions
GENMAT-1 is in a sun-synchronous orbit (SSO), a specialised form of LEO at approximately 455 km altitude. Its 97.4° inclination causes the orbital plane to precess at exactly the rate of the Earth’s revolution around the Sun, so the satellite crosses each latitude at a consistent local solar time. It completes one orbit every 94 minutes, travelling at 27,510 km/h.
GENMAT-1 is operated by GenMat (United States). It is catalogued by the U.S. Space Surveillance Network under NORAD ID 58276. You can track GENMAT-1 in real time on Orbital Radar’s live tracker or browse all operators in the operator directory.
GENMAT-1 was launched on 2023-11-11 from Vandenberg Space Force Base, United States, primarily used for polar and sun-synchronous orbit launches due to its southward ocean trajectory from California. At its current altitude, the estimated remaining orbital lifetime is: ~1–3 years. View the full satellite launch log.
Yes — Orbital Radar tracks GENMAT-1 (NORAD ID 58276) using the latest TLE (two-line element set) orbital data in its live tracking catalogue (see our data sources). Open the live tracker to see its current position, altitude, speed and orbital path updated in real time. You can also browse the satellite directory to find other tracked objects.
GENMAT-1 travels at approximately 27,510 km/h (17,094 mph) — roughly 7.64 km/s. It completes 15.37 orbits per day, meaning the crew or instruments aboard (if any) would experience approximately 31 sunrises and sunsets every 24 hours.